N595AA

Part: HOSE — CRACKED (CREW O2) · airframe 67,934 hrs · 29,149 cycles

SLC INFLIGHT PDX-DFW CREW REPORTED COCKPIT O2 BOTTLE FOUND LEAKING IN FLIGHT. FLIGHT DIVERTED SLC LANDED WITHOUT INCIDENT. REPLACED REGULATOR SUPPLY HOSE. SYSTEM GROUND CHECKED NORMAL OPERATION CLOSED.

Part: DUCT — DAMAGED (AC BAY) · airframe 67,540 hrs · 28,936 cycles

TAIL COMPARTMENT TEMPERATURE HIGH, LIGHT ILLUMINATED. REPLACED DUCT & BOTH OVERHEAT SENSORS. SYSTEM GROUND CHECKED NORMAL.

Part: FMU — MALFUNCTIONED (FIRE WARNING) · airframe 67,533 hrs · 28,930 cycles

MASTER WARNING LIGHT ILLUMINATED WITH CARGO FIRE LIGHT. ALL THREE CARGO FIRE LIGHTS ILLUMINATED ON THE SDS PANEL. EMERGENCY DECLARED FLIGHT RETURNED TUL LANDED WITHOUT INCIDENT. REPLACED CARGO FIRE MAINTENANCE UNIT. SYSTEM GROUND CHECKED NORMAL.

Part: PUMP — INOPERATIVE (HYDRAULIC SYS) · airframe 66,355 hrs · 28,322 cycles

DFW - CREW REPORTED RIGHT HYDRAULIC SYSTEM FAILED. EMERGENCY DECLARED FLIGHT LANDED DFW WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE DRIVEN HYDRAULIC PUMP. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: SPAR — DAMAGED (VERTICAL STAB) · airframe 64,022 hrs · 27,128 cycles

RIGHT VERTICAL STABILIZER, SEVENTH SPAR HOLE ABOVE STATION ZFS 52.267 OUT OF ROUND AND BEYOND LIMITS. INSTALLED DOUBLER TRIPLER PER EA MD80-55-023253 AND / SRM 51-30-10.

Part: FRAME — CRACKED (FUSELAGE) · airframe 63,849 hrs · 27,031 cycles

AFT ACCY 1474 CANT FRAME CRACKED AFT OF LONGERON 18 RIGHT. ACCOMPLISHED DOUBLER REPAIR PER AARD 53-10-00-15.

Part: ENGINE — FAILED (RIGHT) · airframe 59,871 hrs · 25,089 cycles

CREW REPORTED AT ABOUT 13000 FT THERE WAS A LOUD BANG THEN THE RIGHT ENGINE FAILED (SINGLE ENGINE TIME 13 MINUTES). N1 & N2 ROLLED BACK AND TEMPS EXCEEDED 800 DEGREES. FIRE HANDLE WAS PULLED AND THE FUEL SHUT-OFF LEVER WAS ACTUATED TO "OFF" POSITION AND TEMPS FINALLY BEGAN TO SUBSIDE. FOLLOWED QRH PROCEDURES. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. REPLACED RIGHT ENGINE ON 11/11/2010 AT DFW. SYSTEM GROUND CHECK NORMAL OPERTATION.

Part: BEAM — CORRODED (CARGO BAY) · airframe 59,811 hrs · 25,060 cycles

AFT CARGO DOOR BEAM - CORROSION EMITTING FROM UNDERNEATH EXISTING DOUBLER. REMOVED CORROSION AND COMPLETED REPAIR PER EA MD80-53-013555 AND AARD 53-10-00-3.

Part: FRAME — CRACKED (FUSELAGE) · airframe 59,811 hrs · 25,060 cycles

CRACK IN THE FRAME AT STATION 1418 AT LONGERON 2 RIGHT AND LONGERON 2 LEFT. REPAIRED PER SRM 53-03 FIGURE 31A AND EA MD80-53-013742.

Part: SUPPORT — CRACKED (FUSELAGE) · airframe 59,811 hrs · 25,060 cycles

SEAT TRACK SUPPORT BELOW TRACK NUMBER 3 AT STATION 886 IS CRACKED AT LOWER END. INSTALLED DOUBLER STIFFENER PER EA MD-80-53-013587.

Part: FITTING — CRACKED (FUSELAGE) · airframe 59,811 hrs · 25,060 cycles

SHEAR CLIP CRACKED STATION 1437 BETWEEN LONGERONS 2 AND 3 LEFT. INSTALLED NEW SHEAR TIE CLIP PER SRM 51-30-05.

Part: ANGLE — CRACKED (FUSELAGE) · airframe 59,811 hrs · 25,060 cycles

GEAR, NOSE LANDING GEAR, RIGHT CORNER OF FORWARD DOOR CUTOUT, J-ANGLE IS CRACKED THRU FASTENER. STOP DRILLED CRACK AND INSTALLED DOUBLER REPAIR PER AARD 53-10-00-4.

Part: FITTING — CRACKED (FUSELAGE) · airframe 59,811 hrs · 25,060 cycles

SHEAR CLIP CRACKED STATION 1437 BETWEEN LONGERONS 2 AND 3 RIGHT. INSTALLED NEW SHEAR TIE CLIP PER SRM 51-30-05.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,811 hrs · 25,060 cycles

AFT GALLEY SERVICE DOOR, SUBFLOOR AREA HAS CORROSION ON TOPSIDE FROM STATION 1174 TO 1180. INSTALLED REPAIR DOUBLER PER AARD 53-20-00-16.

Part: FRAME — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,811 hrs · 25,060 cycles

FRAME CORRODED AT STATION 1117. REPLACED FRAME PER SRM 51-30-05 AND EA MD-80-51-013637.

Part: FLOOR SUPPORT — CRACKED (FUSELAGE) · airframe 59,811 hrs · 25,060 cycles

FLOORBOARD SUPPORT CRACKED UNDER NUMBER 3 SEAT TRACK STATION 826. REPAIRED PER EA MD80-53-013587.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,811 hrs · 25,060 cycles

NUMBER 6 SEAT TRACK STATION 466 BLENDED OUT OF LIMITS. CUT OUT DAMAGE AND INSTALLED PLUG PER AARD 53-20-00-10 AND EA MD80-53-013636.

Part: VERTICAL SUPPORT — CRACKED (FUSELAGE) · airframe 59,811 hrs · 25,060 cycles

VERTICAL SUPPORT CRACKED AT UPPER END JUST BELOW FLOOR INBOARD OF FORWARD ENTRANCE STAIRWAY DOOR CUT OUT STATION 160 (MARKED). INSTALLED NEW VERTICAL SUPPORT PER SRM 51-30-05 AND 51-30-01.

Part: VERTICAL SUPPORT — CRACKED (FUSELAGE) · airframe 59,811 hrs · 25,060 cycles

SEAT TRACK SUPPORT BELOW TRACK NUMBER 5 AT STATION 927 IS CRACKED AT LOWER END. FABRICATED AND INSTALLED FILLER AND DOUBLER FOR SEAT TRACK SUPPORT BELOW TRACK NUMBER 5 AT STATION 927 PER EA MD80-53-013587.

Part: SEAT TRACK — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,811 hrs · 25,060 cycles

SEAT TRACK NUMBER 2 CORRODED OUT OF LIMITS. INSTALLED NEW SEAT TRACK SECTION PER SRM 51-30-05.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,811 hrs · 25,060 cycles

CENTER FLOORBOARD INTERCOSTAL BETWEEN STATIONS 1271 AND 1287 IS CRACKED. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-05.

Part: INTERCOSTAL — CRACKED (FUSELAGE) · airframe 59,811 hrs · 25,060 cycles

CENTER FLOORBOARD INTERCOSTAL BETWEEN STATION 1287 AND 1309 CRACKED. REMOVED AND REPLACED INTERCOSTAL PER SRM 51-30-05.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 59,811 hrs · 25,060 cycles

BRACKET CRACKED UNDER RIGHT TIE-DOWN TRACK STATION 788. REMOVED AND REPLACED BRACKET PER SRM 53-30-05.

Part: PAN — CORRODED (FUSELAGE) · airframe 59,811 hrs · 25,060 cycles

FORWARD LAVATORY SERVICE PANEL CORRODED AT FORWARD END. REMOVED CORROSION AND INSTALLED DOUBLER REPAIR PER EA MD80-53-013564.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 59,811 hrs · 25,060 cycles

BRACKET CRACKED UNDER LEFT TIE-DOWN TRACK STATION 788. REMOVED AND REPLACED BRACKET PER SRM 53-30-05.

Part: PAN — CORRODED (CARGO BAY) · corrosion level 2 · airframe 59,811 hrs · 25,060 cycles

CORROSION ON FORWARD CARGO DOOR PAN STATIONS 389 TO 408. REMOVED AND REPLACED DOOR PAN PER SRM 53-05-00 FIGURE 44.

Part: SKIN — DAMAGED (AILERON) · airframe 59,811 hrs · 25,060 cycles

RIGHT AILERON LOWER SKIN 21 INCHES FROM INBOARD END HAS A 2 INCH DENT WITH CRUSHED CORE. APPLIED WET LAY-UP AND BAGGED REPAIR PER SRM 51-70-01A FIGURE 34 SHEET 1.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,811 hrs · 25,060 cycles

RIGHT STATIONS 664 TO 668 CORROSION OUT OF LIMITS PER SRM 51-10-03. FABRICATED AND INSTALLED DOUBLER AT RIGHT STATIONS 664 TO 668 PER AARD 53-20-00-16.

Part: BRACKET — CRACKED (FUSELAGE) · airframe 59,811 hrs · 25,060 cycles

BRACKET CRACKED STATION 237 BELOW RIGHT TIE DOWN TRACK BETWEEN LONGERON 27 RIGHT AND LONGERON 28 RIGHT FORWARD CARGO. REMOVED AND REPLACED BRACKET PER SRM 51-30-05.

Part: CUSP WEB — CRACKED (FUSELAGE) · airframe 59,811 hrs · 25,060 cycles

RIGHT STATIONS 984 TO 1003 AFT SIDE OF FORWARD LIGHTNING HOLE CRACKED. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: MOUNT — DAMAGED (FUSELAGE) · corrosion level 2 · airframe 59,811 hrs · 25,060 cycles

G-1 GALLEY FORWARD CENTER MOUNT HAS CORROSION. INSTALLED NEW G1 CENTER GALLEY MOUNT PER SRM 51-30-05.

Part: STRIP — LOOSE (RT WING) · airframe 59,811 hrs · 25,060 cycles

RIGHT WING STAINLESS WEAR STRIP LOOSE AT INBOARD END OF NUMBER 2 SLAT. RIGHT WING FILLED WORN AREA WITH DEVCON F, INSTALLED TITANIUM DOUBLER AND REINSTALLED STRIP PER EA MD60-27-013560 DATED 10-15-10.

Part: RIB — CRACKED (LE SLAT) · airframe 59,811 hrs · 25,060 cycles

RIGHT NUMBER 5 OUTBOARD SLAT OUTBOARD RIB HIGH FREQUENCY EDDY CURRENT INSPECTION INDICATES A CRACK. REPLACED DAMAGED NUMBER 15 RIB OUTBOARD ON SLAT WITH A NEW ONE PER IAW ESO 80117.

Part: CUSP WEB — CORRODED (FUSELAGE) · corrosion level 2 · airframe 59,811 hrs · 25,060 cycles

RIGHT STATIONS 535 TO 545 CORROSION OUT OF LIMITS PER SRM 51-10-03. INSTALLED DOUBLER PER AARD 53-20-00-16.

Part: RIB — CRACKED (LE SLAT) · airframe 59,811 hrs · 25,060 cycles

RIGHT NUMBER 5 SLAT 2ND FROM OUTBOARD RIB HIGH FREQUENCY EDDY CURRENT INSPECTION INDICATES A CRACK. REPLACED DAMAGED NUMBER 14 RIB 2ND OUTBOARD ON SLAT WITH A NEW ONE PER IAW ESO 80117.

Part: DIAPHRAGM — GOUGED (FUSELAGE) · airframe 59,811 hrs · 25,060 cycles

GOUGE IN SUB-FLOOR STATION 171. REPAIR DOUBLER INSTALLED PER AARD 53-20-00-16.

Part: SKIN — DAMAGED (TE FLAP) · airframe 59,811 hrs · 25,060 cycles

RIGHT WING INBOARD TRAILING EDGE FLAP LOWER SURFACE HAS SMALL DENT AND GOUGE LOCATED 3 FEET OUTBOARD OF WING ROOT IN CENTER OF FLAP, ALSO .75 INCH GOUGE AND SCRATCH WITHIN SRM LIMITS LOCATED 3 FEET OUTBOARD OF WING ROOT. RIGHT WING INBOARD TRAILING EDGE FLAP REPLACED DAMAGED LOWER SKIN WITH NEW SKIN AS PER ESO 80095.

Part: DIAPHRAGM — GOUGED (FUSELAGE) · airframe 59,811 hrs · 25,060 cycles

2 EACH GOUGES IN SUB FLOOR STATION 180 FORWARD OF NUMBER TWO SEAT TRACK. REPAIR DOUBLER INSTALLED PER AARD 53-20-00-16.

Part: DIAPHRAGM — GOUGED (FUSELAGE) · airframe 59,811 hrs · 25,060 cycles

2 EACH GOUGES IN SUB FLOOR STATION 193 FORWARD OF NUMBER TWO SEAT TRACK. REPAIR DOUBLER INSTALLED PER AARD 53-20-00-16.

Part: SKIN — DENTED (LE SLAT) · airframe 59,811 hrs · 25,060 cycles

RIGHT WING DENT RIGHT NUMBER 1 SLAT AT UPPER SURFACE 12 INCHES FROM INBOARD SIDE. RIGHT WING REWORKED DENTED AREA TO BE WITHIN LIMITS, DYE CHECKED AREA, NO CRACKS FOUND PER ESO 80117.

Part: STOP FITTING — CRACKED (FUSELAGE) · airframe 59,811 hrs · 25,060 cycles

AFT CABIN VAULT DOOR OPENING. LOWER LEFT DOOR STOP FITTING IS CRACKED ALONG LOWER RADIUS ON AFT SIDE. NEW FITTING INSTALLED PER SRM 51-01-00.

Part: SKIN — DAMAGED (AILERON) · airframe 59,811 hrs · 25,060 cycles

RIGHT AILERON LOWER SKIN 21 INCHES FROM INBOARD END HAS A 2 INCH DENT WITH CRUSHED CORE. RIGHT AILERON REMOVED CRUSHED CORE AND REPLACED CORE. APPLIED WET LAY-UP AND BAGGED REPAIR PER SRM 51-70--01A FIGURE 34 SHEET 1.

Part: PAN — CRACKED (WINDOW) · airframe 59,811 hrs · 25,060 cycles

CRACK AT LOWER FORWARD TAB OF CABIN WINDOW PAN AT STATION 1098. REPAIR DOUBLER INSTALLED PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 59,811 hrs · 25,060 cycles

CRACK AT UPPER FORWARD CORNER OF CABIN WINDOW PAN STATION 946. REPAIR DOUBLER INSTALLED PER AARD 53-10-00-25.

Part: PAN — CRACKED (WINDOW) · airframe 59,811 hrs · 25,060 cycles

CRACK IN UPPER FORWARD TAB OF CABIN WINDOW PAN STATION 807. REPAIR DOUBLER INSTALLED PER AARD 53-10-00-25.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,560 hrs · 24,941 cycles

EMERGENCY LIGHTS AT RIGHT AND LEFT NUMBER DOORS INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHTS AT RIGHT AND LEFT NUMBER 1 DOORS. OPS CHECK NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 59,560 hrs · 24,941 cycles

FLOOR PROXIMITY EMERGENCY PATH LIGHTS FROM ROWS 3 TO 19 INOPERATIVE. REPLACED BATTERY PACK FOR FLOOR PROXIMITY EMERGENCY PATH LIGHTS AT ROWS 3 TO 19. OPS CHECK NORMAL.

Part: LIGHT — INOPERATIVE (CABIN) · airframe 58,306 hrs · 24,346 cycles

EMERGENCY LIGHTS ABOVE THE CATWALK AT DOOR INOPERATIVE. REPLACED LAMP FOR AFT ASSOCIATED EMERGENCY LIGHTS. OPS CHECKED NORMAL.

Part: BATTERY PACK — DISCHARGED (CABIN) · airframe 58,306 hrs · 24,346 cycles

EMERGENCY LIGHTS ABOVE THE CATWALK AT DOOR INOPERATIVE. REPLACED EMERGENCY LIGHT BATTERY PACK. OPS CHECKED NORMAL.

Part: HEATER — FAILED (PITOT/STATIC SYS) · airframe 58,060 hrs · 24,231 cycles

ELP - INFLIGHT SJC-DFW. CAPTAINS PITOT HEATER FAILED IN FLIGHT. FLIGHT UNABLE TO CONTINUE DUE TO ICING IN THE DFW AREA. FLIGHT DIVERTED ELP LANDED WITHOUT INCIDENT. REPLACED CAPTAINS PITOT STATIC. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: CLEVIS — BROKEN (AIRSTAIRS) · airframe 57,699 hrs · 24,083 cycles

DFW - CREW REPORTED A LOUD BANG IN THE FORWARD FUSELAGE AREA FOLLOWED BY ERRATIC PRESSURIZATION CONTROL. EMERGENCY DECLARED RETURNED DFW LANDED WITHOUT INCIDENT. AIRCRAFT REMOVED FROM SERVICE. FOUND THAT THE FORWARD EDGE OF THE PASSENGER ENTRANCE STAIRS DOOR BELOW THE LEFT NUMBER 1 DOOR WAS STICKING OUT DUE TO A BROKEN CLEVIS THAT CONNECTS THE DOOR TO THE LATCHING MECHANISM. REPLACED FORWARD CLEVIS BRACKET. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: SKIN — DAMAGED (DOOR) · airframe 56,647 hrs · 23,646 cycles

OUTER SKIN ON DOOR HAS EXCESSIVE DAMAGE TO AFT RIGHT CORNER. REMOVED DAMAGED SKIN, FABRICATED AND INSTALLED NEW SKIN PER ESO 80178 AND SRM 52-40-0.

Part: ACTUATOR — INOPERATIVE (NLG STEERING) · airframe 56,096 hrs · 23,385 cycles

IND - ON TAKEOFF ROLL IN DFW, AIRCRAFT PULLED EXCESSIVELY TO RIGHT, AIRCRAFT CONTROLLED TAKEOFF ROLL AND DEPARTED NORMALLY. ON APPROACH WHEN LANDING GEAR WAS IN DOWN POSITION NOSE GEAR INDICATION DID NOT SHOW GREEN. CREW ACCOMPLISHED A TOWER FLY-BY TO CONFIRM GEAR DOWN. REPLACED RIGHT NOSE LANDING GEAR STEERING ACTUATOR AND STEERING CONTROL VALVE. REPLACED NOSE LANDING GEAR INDICATOR BULBS. SYSTEM GROUND CHECK NORMAL OPERATION.

Part: ANGLE — CORRODED (ZONE 100) · corrosion level 2 · airframe 55,492 hrs · 23,104 cycles

MID CARGO, CORROSION ON ANGLE AT STATION 665 RIGHT SIDE. INSTALLED DOOR BEAM DOUBLER PER AARD 53-10-00-3.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

DFW - OVERHEAD EMERGENCY LIGHTS AT AFT CATWALK INOPERATIVE. REPLACED BATTERY PACK AT AFT CATWALK.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

DFW - OVERHEAD EMERGENCY LIGHTS FROM ROWS 12 THRU 15 ARE DIM. REPLACED BATTERY PACK AT ROW 12 THRU 15.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

DEF - OVERHEAD EMERGENCY LIGHT AT AFT ENTRY AISLE INOPERATIVE. REPLACED BATTERY PACK AT AFT ENTRY AISLE.

Part: BATTERY PACK — DISCHARGED (EMERGENCY LIGHTS)

DFW - AFT FACING TAIL CONE RAMP EMERGENCY LIGHTS INOPERATIVE. REPLACED BATTERY PACK AT AFT FACING TAIL CONE RAMP.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LGIHT)

BOS - CEILING EMERGENCY LIGHTS AT ROW 14 INOPERTIVE. REPLACED BATTERY PACK FOR CEILING EMERGENCY LIGHTS AT ROW 14. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — INOPERATIVE (EMERGENCY LIGHT)

LGA - EMERGENCY LIGHT AT SEAT ROW 24 INOPERATIVE. REPLACED BATTERY PACK FOR EMERGENCY LIGHT AT SEAT ROW 24. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: CHARGER — INOPERATIVE (EMERGENCY LIGHT)

EMERGENCY LIGHTS IN CEILING BETWEEN AFT LAVATORIES INOPERATIVE. REPLACED BATTERY CHARGER ASSEMBLY FOR EMERGNECY LIGHTS IN CEILING BETWEEN AFT LAVATORIES. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: BATTERY PACK — DISCHARGED (CABIN)

DFW - B2-28 BATTERY PACK INOPERATIVE. REMOVED AND REPLACED B2-28 BATTERY PACK PER MM. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: WIRE — DAMAGED (A/C BAY)

DFW - AFT CATWALK EMERGENCY LIGHTS INOPERATIVE. REPLACED WIRING FROM TAIL CONE LIGHT TO AFT CATWALK EMERGENCY LIGHTS. SYSTEM GROUND CHECKED NORMAL OPERATION.

Part: DUCT — FAILED (RT ENGINE)

EN ROUTE DFW-MEX, DURING CLIMB-OUT AT APPROXIMATELY 14,000 FT, RT ENGINE FIRE LIGHT ILLUMINATED WITH AURAL WARNING. BOTH LOOP LIGHTS WERE ILLUMINATED, EGT REACHED APPROXIMATELY 520 DEGREES. ENGINE WAS RETARDED TO IDLE. RETURNED AND LANDED DFW WITHOUT INCIDENT. VISUAL INSPECTION BY FIRE CREW REVEALED NO FIRE OR DAMAGE. ENGINE WAS THEN SHUTDOWN DURING TAXI IN. REPLACED RIGHT ENGINE ANTI-ICE DUCT. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: FRAME — WORN (FUSELAGE)

TUL - FOUND DEEP WEAR ON FRAME AT STATION 1401 AT LONGERON 21R. REPAIRED FRAME AT 1401 AND LONGERON 21R PER ESO 80599. (M)

Part: DOOR FRAME — CORRODED (FUSELAGE)

TUL - FOUND AFT CARGO DOOR, LOWER FRAME CORRODED FROM STATION 1155 TO 1216. BLENDED CORROSION AND INSTALLED DOUBLER PER AARD 53-10-00. (M)

Part: SKIN — CRACKED (FUSELAGE)

TUL - FOUND FUSELAGE SKIN CRACKED STATION 1380 LONGERON 14L. INSTALLED DOUBLER PER AARD 53-30-00-02. (M)

Part: SKIN — DENTED (FUSELAGE)

TUL - FOUND DENT IN FUSELAGE SKIN AT STATION 237 L19 LEFT. CUT OUT DAMAGED AREA OF SKIN AND INSTALLED REPAIR PER SRM 53-04 FIG 12B. (M)

Part: SEAT TRACK — CORRODED (FUSELAGE)

FOUND PITTING CORROSION IN BASE OF SEAT TRACK NR 3 FROM STATION 658 TO STATION 672. ROUTED OUT DAMAGED AREA AND INSTALLED PLUG AS REQUIRED PER AARD 53-20-00-10. (M)

Part: LIGHT — INOPERATIVE (CABIN)

DFW - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT SEAT 17D INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: LIGHT — INOPERATIVE (TAILCONE)

LAX - DURING OVERNIGHT MAINTENANCE, EMERGENCY EXIT LIGHT AT TAIL CONE INOPERATIVE. REPLACED EMERGENCY EXIT LIGHT ASSEMBLY. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: BATTERY PACK

LAX - DURING OVERNIGHT MAINTENANCE, TAIL COMPARTMENT EMERGENCY EXIT LIGHTS FAILED TEST. REPLACED BATTERY PACK. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: WARNING SYSTEM — ACTIVATED (COCKPIT)

ORD - FLT 1091 - EN ROUTE ORD-DEN, SHORTLY AFTER TAKEOFF DETECTED TAIL COMPARTMENT HIGHT TEMPERATURE LIGHT ILLUMINATE IN COCKPIT. INSPECTED TAIL COMPARTMENT TEMPERATURE HIGH LIGHT COMPONENTS. NO DEFECTS FOUND. TIGHTENED TAIL ANTI-ICE VALVE B-NUT. TIGHTENED LEFT SIDE PRESSURE REGULATOR CLAMPS PER THE MM. ACCOMPLISHED LEFT SIDE AUGMENTATION VALVE CLAMP TORQUE. ACCOMPLISHED REQUIRED LEAK CHECKS PER THE MM. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)

Part: EEL STRIP — DEFECTIVE (CABIN)

RDU - DURING OVERNIGHT CHECK, EMERGENCY FLOOR LIGHTS BETWEEN PASSENGER SEAT ROWS 21DEF AND 29DEF FOUND INOPERATIVE. REPLACED EMERGENCY FLOOR LIGHT STRIP BETWEEN PASSENGER SEAT ROWS 21DEF AND 29DEF. SYSTEM GROUND CHECK NORMAL OPERATION. (X)

Part: EEL WIRE — DEFECTIVE (CABIN)

DFW - DURING OVERNIGHT CHECK, AFT CABIN EMERGENCY EXIT FLOOR PATH LIGHTS INOPERATIVE. REPAIRED WIRING AND REPLACED BATTERIES. SYSTEM GROUND CHECKED NORMAL OPERATION. (M)